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Aircraft record

N761PH1981 Sikorsky S-76A

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Aug 30, 2017.

Safety record in brief:No NTSB accidents or incidents since 198218 ADs may apply36 service difficulty reports

Registration
Deregistered
Last based in
Lafayette, LA
owner city / state
Engine
ARRIEL 1SER · 681 hp
Turbomeca
Owners
1
since 2002
NTSB events
None
since 1982
ADs may apply
18
confirm with A&P
Service reports
36
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Phi INC
Owner type
Corporation
City, state
Lafayette, LA
Certificate issued
May 10, 2002
Canceled
Aug 30, 2017
Airworthiness
Standard · Transport
Airworthiness date
Dec 22, 2000

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Sikorsky
Model
S-76A
Year
1981
Serial number
760224
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
14
Engines
2
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
H1NE
Mode S code
AA468C

Engine

Make and model
Turbomeca Arriel 1ser
Type
Turbo-shaft
Power
681 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2002 – 2017Phi INCLafayette, LA

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (18)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2024-20-07Various HelicoptersDec 5, 2024Airframe (S-76A)Only with: Only helicopters modified by the applicable STC (SR00831LA, SR00780LA, SR01687LA, SR00856LA, SR01855LA, SR02244LA, SR01779LA, SR01459LA, SR01535LA, SR00932LA, SR02049LA, SR02484LA, or SR01902LA).
2017-19-01Sikorsky Aircraft Corporation HelicoptersJan 2, 2018Airframe (S-76A)Certain serial numbers: …–761075. Only with: Main rotor servo pushrod assembly P/N 76400-00034-059, 76400-00014-074, 76400-00014-076, or 76400-00014-077 installed.
2015-26-10Sikorsky Aircraft Corporation HelicoptersFeb 9, 2016Airframe (S-76A)Only with: Main gearbox P/N 76351-09000 series, 76351-09500 series, or 76351-09600 series installed that has been repaired in accordance with Sikorsky ORI No. 76350-065 (original or Revision A).
2015-19-51Sikorsky Aircraft Corporation HelicoptersNov 10, 2015Airframe (S-76A)Only with: Main rotor servo input control pushrod assembly P/N 76400-00034-059 or tail rotor pushrod assembly P/N 76400-00014-071 installed.
2013-22-15Sikorsky Aircraft Corporation (Sikorsky) HelicoptersDec 13, 2013Airframe (S-76A)Certain serial numbers: …–760822. Only with: With spindle cuff assembly P/N 76102-08001-043, -045 or -046, or blade fold cuff assembly P/N 76150-09601-041 installed.
Show all 18 ADs
ADSubjectEffectiveApplies to
2012-15-08Sikorsky Aircraft Corporation HelicoptersSep 21, 2012Airframe (S-76A)Only with: Electric rotor brake (ERB) P/N 76363-09100-012 installed.
2010-26-09Sikorsky Aircraft Corporation (Sikorsky) Model S76A, B, and C HelicoptersJan 12, 2011Airframe (S-76A)Only with: LITEF LCR-100 Attitude Heading and Reference System (AHRS) Unit P/N 145130-7100 installed
2010-10-02Sikorsky Aircraft Corporation Model S-76A, B, and C HelicoptersJun 17, 2010Airframe (S-76A)Only with: Main rotor servo actuator Sikorsky P/N 76650-09805-109 or -110 (also marked HR Textron or Woodward HRT P/N 3006760-109 or -110) installed.
2005-22-01Sikorsky Aircraft Corporation Model S-76A, B, and C HelicoptersNov 10, 2005Airframe (S-76A)Only with: Main rotor hub pilot fitting P/N 76103-08003-101 with 1500 or more hours TIS installed.
2003-04-15Sikorsky Aircraft Corporation Model S-76A, B, and C HelicoptersFeb 27, 2003Airframe (S-76A)
2002-15-51Sikorsky Aircraft Corporation Model S76A, B, and C HelicoptersOct 18, 2002Airframe (S-76A)
2001-10-06Sikorsky Aircraft Corporation Model S-76A, S-76B, and S-76C HelicoptersMay 17, 2001Airframe (S-76A)Only with: Main rotor shaft assembly P/N 76351-09030 (all dash numbers) installed.
94-14-20 R1Sikorsky Aircraft Corporation Model S-76A HelicoptersJun 8, 2001Airframe (S-76A)Only with: Tail rotor blade assembly P/N 76101-05001 (all dash numbers) or 76101-05101 (all dash numbers) installed with more than 130 hours time-in-service.
2001-01-04Sikorsky Aircraft Corporation Model S-76A, S-76B, and S-76C HelicoptersFeb 2, 2001Airframe (S-76A)Certain serial numbers: …–760513. Only with: Positioning rod assembly P/N 1945E-31A or 2071-31, or side brace rod end P/N 1945E-235 or 2071-235, installed.
2000-11-52Sikorsky Aircraft Corporation Model S-76 Series HelicoptersAug 31, 2000Airframe (S-76A)
2000-12-09Sikorsky Aircraft Corporation (Sikorsky) Model S-76A HelicoptersJul 28, 2000Airframe (S-76A)Only with: Aero Aire Air Conditioning System P/N S-76A-1-2 installed, modified in accordance with STC SH4680SW.
99-19-30Sikorsky Aircraft Corp. Model S76A, B, and C HelicoptersOct 4, 1999Airframe (S-76A)
99-11-04Sikorsky Aircraft Model S-76A HelicoptersJul 9, 1999Airframe (S-76A)Only with: Turbomeca Arriel 1S1 engines installed in accordance with STC SH568NE, including drawing number 76070-30601.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (36)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Landing gear · connector · dirtyNov 12, 2009

    ON LANDING, LANDING GEAR WOULD NOT EXTEND. USED CHECKLIST AND NOTIFIED MX. LANDING GEAR CAME DOWN AND LOCKED AFTER RAISING AND LOWERING THE HANDLE A FEW TIMES. MX CLEANED CONTROL PANEL AND PANEL CONNECTOR P5 AND RT WHEEL CONNECTOR P224 AND CONNECTOR AT CONTROL VALVE J222. JACKED ACFT AND CYCLED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · squat switch · out of adjustJan 2, 2006

    AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. MAINTENANCE ADJUSTED THE RIGHT HAND WEIGHT ON WHEELS SWITCH.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · downlock · false indicationNov 15, 2005

    TEN MINUTES OUT, AN AIRCRAFT REPORTED THAT ONE MAIN LANDING GEAR WAS DOWN OR PARTIALLY DOWN. SLOWED TO 130 KTS AND FLEW BY TOWER AND THEY CONFIRMED THE LT MAIN GEAR WAS DOWN. COCKPIT INDICATIONS SHOWED GEAR UP AND LOCKED. LOWERED LANDING GEAR AND GOT INDICATION OF ALL GEAR DOWN AND LOCKED.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Engine · engine · failedJan 25, 2004

    WHILE IN CRUISE FLIGHT HEARD A BUMP, THE AIRCRAFT YAWED, NR 1 ENGINE OUT LIGHT CAME ON, MAST CAUTION LIGHT CAME ON, ENGINE CHIP LIGHT CAME ON, AND ALL GAUGES WENT TO ZERO ON THE NR 1 ENGINE. CONTINUED FLIGHT AND LANDED AT AIRPORT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Tail rotor · blade · wornJul 12, 2003

    PRIMARY RUBBER ON THE LEADING EDGE HAS ERODED TO THE FIBERGLASS SKIN AND WIRE MESH OF TAIL ROTOR BLADE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Tail rotor · blade · erodedJul 12, 2003

    PRIMARY RUBBER ON THE LEADING EDGE HAS ERODED TO THE FIBERGLASS SKIN AND WIRE MESH OR TAIL ROTOR BLADE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Autoflight · actuator · roughJul 9, 2003

    WORN AND CORRODED. REPLACED CLUTCH WASHER A7683361 DUE TO WORN; ROD END BEARING MS21151-8C DUE TO ROUGH; POTENTIOMETER (2 EA) A768343-3 DUE TO WORN. REPAIRED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Autoflight · actuator · corrodedJul 9, 2003

    AFCS ACTUATOR WORN AND CORRODED. REPLACED CLUTCH WASHER A768336-1 DUE TO WORN; ROD END BEARING MS21151-8C DUE TO ROUGH; POTENTIOMETER (2 EA) A768343-3 DUE TO NULL IN CENTER. REPAIRED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor · tip cap · debondedJun 21, 2003

    THE "C" CHANNEL HAS SOME DEBONDING AND THE TOP OUTSIDE DOUBLER SEPERATED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor · tip cap · separatedMay 22, 2003

    THE CRESENT SHAPE DOUBLER UPPER AND LOWER SIDE IS SEPARATED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 36 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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